• Proceedings of the Korean Institute of Navigation and Port Research Conference
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• 2013.06a
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• pp.105-107
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• 2013

위성항법 기반 위치정보 서비스에 대한 안정성 및 신뢰성 확보를 위해서는 위성신호의 이상 감시가 필수적이며, 특히 안전과 관련된 응용분야에서의 위성신호 이상은 안전사고와 직결될 수 있으므로 위성신호 감시는 상시 안정적으로 운용되어야 한다. 따라서 효율적인 이상감시 기법 설계와 다양하고, 지속적인 시험평가를 위해서는 테스트베드 구축이 필요하며, 테스트베드 구축을 위한 요소 중 특히, 다양한 시나리오의 신호 이상을 생성할 수 있는 이상신호 생성 기술이 필요하다. 따라서 본 논문에서는 다양한 이상신호 생성 및 실신호 특성 반영이 가능한 소프트웨어 기반 GPS 이상신호 생성기를 제안한다. 소프트웨어 기반 GPS 이상신호 생성기는 높은 확장성을 가지므로, 사용자가 적용 및 응용하기 쉬우며, 상용 신호생성 시뮬레이터와 비교하여 실신호 특성을 반영한 이상신호 생성이 가능하다.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.46 no.7
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• pp.592-601
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• 2018

The GPS/INS integrated navigation system, which is one of the electronic equipments mounted on military aircraft store, can not directly receive GPS signals by the aircraft wing before the drop, so GPS navigation data is received from the aircraft and used for filter integration, afterwards, the integrated navigation is performed using the GPS information directly received through the antenna. In this case, it is possible to operate the mount in old aircraft without any modification of the aircraft when GPS data is transmitted using wireless. However, the delay occurs while the aircraft navigation data is transmitted to the integrated navigation filter of the aircraft store via wireless, which affects the time synchronization of the GPS measurement and the INS information, affecting the integrated navigation performance. In this paper, an algorithm to analyze and compensate the effect of generation and transmission delay that can occur when implementing GPS/INS integrated navigation system of aircraft store that receives GPS data via wireless.

• Bulletin of the Korean Space Science Society
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• 2007.10a
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• pp.63.2-63.2
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• 2007

• Journal of the Korea Institute of Military Science and Technology
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• v.11 no.3
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• pp.30-39
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• 2008

An artificial vision aided NDGPS/INS system has been developed and tested in the dynamic environment of ground and flight vehicles to evaluate the overall system performance. The results show the significant advantages in position accuracy and situation awareness. Accuracy meets the CAT-I precision approach and landing using NDGPS/INS integration. Also we confirm the proposed system is effective enough to improve flight safety by using artificial vision. The system design, software algorithm, and flight test results are presented in details.

• Journal of Cadastre & Land InformatiX
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• v.46 no.1
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• pp.133-148
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• 2016

Voices demanding a revision of the aviation law on the operating drones are continuously rising high with the increase of their applicability in various industry fields. According to the current regulations, drones are permitted to fly under very strict conditions, which include limited places and the line-of-sight visibility from pilots. Because of the strict regulations, it is almost impossible for drones to be used in many industries such as parcel delivery services. To improve the business value of drones, we have to improve the accuracy of drones' positions and provide the proper protection levels in order to detect and avoid any risks including the collisions with the other drones. SBAS(Satellite Based Augmentation System) can support the aviation requirements with the accuracy and integrity so as to reduce the position errors and to calculate the protection levels of drones. In this paper, we assign the flight heights of drones according to the decision heights as per LAAS(Local Area Augmentation System) landing categories and conduct a simulation to predict the SBAS available time of the day.

• The Journal of the Korea institute of electronic communication sciences
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• v.9 no.2
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• pp.195-202
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• 2014

The Global Positioning System (GPS), which has various military and commercial applications, is designed to estimate the location of the specific user or object. In order to accurately estimate the location, GPS requires at least four satellite signals. The GPS receiver operates on extremely low signal-to-noise ratio (SNR) environment and it may suffer from various interference signals with the extremely high power. In this paper, we introduce a blind adaptive receiver based on the modified despreader, which suppress interference signals and detect GPS signals of interest without requiring explicit angle-of-arrival (AOA) information. We, also, provide the mathematical analysis for the signal-to-interference and noise ratio (SINR) of the modified despeader beamformer output. A representative computer simulation example is presented to illustrate the interference suppression performance of the considered GPS receiver and mathematical analysis of the SINR.

• Proceedings of the Korean Institute of Navigation and Port Research Conference
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• 2013.10a
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• pp.372-373
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• 2013

위성항법시스템(GNSS)에 대한 전파교란에 대응하기 위한 보완항법시스템인 eLoran은 고출력의 지상파를 사용하기 때문에 전파교란이 현실적으로 힘들다는 장점이 있다. eLoran 신호는 세계표준시(UTC)에 동기화 되어있어서 송신 출력에 따라 실내와 같이 GNSS 신호의 수신이 힘든 경우에도 정확한 시각(timing) 정보를 제공할 수 있다. eLoran을 이용한 시각 정보 제공은 미국 국방부(DoD)에서도 최근에 많은 관심을 보이고 있다. 또한 eLoran은 자체 데이터 채널을 보유하고 있어서 eLoran 보정 신호를 전송할 수 있고, 전파기만에 대비하여 eLoran 신호인증 기법을 적용할 수 있다. 전파교란의 영향을 받지 않고 데이터를 전송할 수 있기 때문에 안정적인 데이터 전송이 필요한 각종 분야에서 eLoran 데이터 채널의 활용이 가능하다. 현재 우리나라는 GNSS를 보완하는 위치 항법 시각(PNT) 시스템으로써 2018년 정상 운용을 목표로 eLoran 시스템 구축 사업을 진행하고 있다.

• Proceedings of the Korean Institute of Navigation and Port Research Conference
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• v.2
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• pp.475-478
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• 2006

본 논문에서는 소형 무인항공기의 정확한 위치, 속도, 자세 정보를 제공하기 위해 저급의 MEMS IMU를 이용한 항법 시스템을 제안한다. 제안하는 시스템은 비행체의 직선운동과 회전운동을 측정할 수 있는 관성측정기와 위성신호를 수신하여 항체의 위치, 속도 정보를 제공하는 GPS 수신기, 지구 자기장 정보를 이용하여 방향각 정보를 제공하는 지자기 센서들로 구성되었다. SDINS와 약결합 방식의 칼만필터를 이용한 항법 시스템은 초기정렬 알고리즘과 센서 오차 보상 알고리즘, 자력계 보상 알고리즘 및 복합항법 알고리즘으로 나뉘며, 설계된 항법 알고리즘들은 시뮬레이션과 차량 실험을 통해서 성능을 분석하였다.

• Journal of Positioning, Navigation, and Timing
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• v.13 no.4
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• pp.497-503
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• 2024

In preparation for cases where Unmanned Aerial Vehicles (UAVs) are abused for surveillance or terrorism, this study proposes a technique to guide a UAV to a target point using a spoofing signal that interferes with the Global Navigation Satellite System (GNSS). However, the waypoint estimation-based approach used in spoofing requires repetitive computations, making real-time processing challenging and reducing its responsiveness to target point changes. This paper proposes a technique that uses reinforcement learning to guide UAV spoofing paths in real time by dynamically learning and adapting to changes in flight states without the need for waypoint estimation. To effectively learn real-time flight state change data, the Advantage Actor-Critic (A2C) reinforcement learning model is utilized. In the simulation, a spoofing path guided simulation that controls flight in real time through reinforcement learning was developed. The proposed reinforcement learning model was applied, and the reinforcement learning model was verified through a simulation experiment where the target point of guided spoofing was changed.

• The Journal of Korean Institute of Communications and Information Sciences
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• v.19 no.8
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• pp.1464-1474
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• 1994

GPS(Global Positioning System)is a satellite-based navigation system that we can survey where we are, anywhere and anytime. In this paper, delay-lock loop of the receiver which detects the navigation data is theoretically analyzed, and designed using the digital logic circuit. Also logic operations for the synchronization are analyzed. The designed system consists of the correlator which correlates the received C/A code and the generated C/A code in the receiver, the C/A code generator which generates C/A code of selected satellite, and the direct digital clock syntheizer which generates the clock of the C/A code generator to control the C/A code phase and clock rate. From the analyses results of the proposed digital delay-lock loop system, the system has the detection propertied over 90% when its input signal power is above-113.98dB. The influence of input signal variation of digital delay loop, which is the input of A/D converter, is investigated and the performance is analyzed with the variation of threshold level via the computer simulation. The logic simulation results show that the designed system detects precisely the GPS navigation data.